N763CX

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 92,380 hrs · 41,718 cycles

CORRODED STRINGER 36L

Part: PRESSURE SWITCH — FAULTED (SLAT SYSTEM) · airframe 90,887 hrs · 41,495 cycles

ON FINAL APPROACH LEADING EDGE SLAT DISAGREE EICAS MESSAGE ANNUNICATED, LANDING ABORTED. CREW PERFORMED GO AROUND AND LEADING EDGE SLAT DISAGREE MESSAGE NO LONGER ANNUNCIATED WHEN FLAPS RETRACTED TO 20. ON SECOND APPROACH, GEAR DISAGREE EICAS MESSAGE AND GEAR LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. PRECAUTIONARY EMERGENCY DECLARED. LANDING ABORTED. WITH GEAR RETRACTED MESSAGE NO LONGER ANNUNICATED. PERFORMED GO AROUND AND TOWER VERIFIED 3 GEAR DOWN. ON THIRD APPROACH, NORMAL LEADING EDGE SLAT AND LANDING GEAR OPERATIONS. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. PSEU AND FSEU BITE CHECKS GOOD. NO FAULTS RECORDED. FURTHER TROUBLESHOOTING IAW B767 FIM 29-11-FT813, ISOLATED INTERMITTENT FAULT TO AIR DRIVEN PUMP. SYSTEM DEFERRED AND TRACKING TO #26756 MEL CAT C. AIRCRAFT RELEASED TO SERVICE. REMOVED AND REPLACED AIR DRIVEN PUMP CONTROL PRESSURE SWITCH S29 IAW B767 AMM 29-11-19. OPERATIONAL AND LEAK TEST GOOD IAW B767 AMM 29-11-00. THIS ACTION CLEARS DEFERRAL-26756

Part: SKIN — SCRATCHED (BS 1356-1363) · corrosion level 2 · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 MAINTENANCE IDENTIFIED D-15 DOT 163 AFT CARGO FUSELAGE SKIN SCRATCHED BETWEEN STATION 1356 AND 1363 AND STRINGERS 31L TO 33L. MATERIAL THICKNESS IAW B767-200 SRM 53-60-01 OUT OF LIMITS. AFT CARGO REPAIRED ON FUSELAGE SKIN BETWEEN STA 1356 AND 1363 AND STRINGERS 331L TO 33L IAW ENGINEERING DOC-21010-3 REV 1R

Part: SKIN — DAMAGED (BS522-566 S28-34) · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. DAMAGE TO FUSELAGE SKIN SECTION 43 BETWEEN STA 522 AND STA 566, BETWEEN STR 28R TO 34R . ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SECTION 43 BETWEEN STATION 522 TO STATION 566 BETWEEN STRINGERS 28R TO 34R IAW ENGINEERING ORDER 21010 REV B.

Part: STRINGER — CORRODED (BS1361-1336 S36L) · corrosion level 2 · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 STRINGER REPAIR DISCOVERED ADDITIONAL CORROSION TO STRINGER 36L 1361 TO 1336. REPAIRED STRINGER 36L ON BS 1361-1336 IAW BOEING 767-200 STRUCTURES REPAIR MANUAL 53-00-03.

Part: STRINGER — CORRODED (BS 1540 S37R) · corrosion level 2 · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 DOT 14 DOT 045 UNDERNEATH WASTE TANK VAVLE AT FS 1540-1582 BETWEEN STRINGER 37L AND 37R CORROSION OUT OF LIMITS ON STRINGER 37R AT STATION 1540. REPAIRED STRINGER 37R ON BS 1540 TO 1582 IAW B767-200 SRM 53-00-03.

Part: PLENUM — CRACKED (APU) · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-24-031-01-01, MAINTENANCE IDENTIFIED SEVERAL CRACKS IN SUPPORT PLATFORM. REMOVED AND REPLACED APU PLENUM IAW BOEING 767-200 STRUCTURES REPAIR MANUAL 51-40-02. APU PLENUM REPAIRED IAW B767-200 STRUCTURES REPAIR MANUAL 53-00-3.

Part: STRINGER — CRACKED (BS 1359 S31L) · airframe 89,978 hrs · 41,088 cycles

AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD 53-552-0101, MAINTENANCE IDENTIFIED D-15 DOT 162 AFT CARGO HAS TWO STRINGERS WITH MARKS AT STATION 1359 STRINGER 31 L AND STATION 1361 STRINGER 33L. DAMAGE REMOVED .028. OUT OF LIMITS IAW B767 SRM 53-00-03. FABRICATED AND INSTALLED STRINGER. REPAIR ON BS 1361 STRINGER 31L IAW B767-200 SRM 53-00-03.

Part: STRUCTURE — PUNCTURED · airframe 86,291 hrs · 39,683 cycles

PRE DEPARTURE-PUNCTURE AFT OF LOWER CARGO DOOR BETWEEN S28R-S29R. AOG. COMPLIED WITH CONDITIONAL INSPECTION IAW B767 AMM 05-51-59/ NO FURTHER DEFECTS NOTED. TEMP REPAIRS IAW ATI ENGINEERING ORDERS 53-767-6676 COMPLIED WITH. ACFT HAS BEEN AUTHORIZED A 1 TIME FERRY FLIGHT TO HOMEBASE FOR PERFORMANCE REPAIRS. AIRCRAFT GROUNDED.

Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 85,902 hrs · 39,542 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 57-564-00-02- RIGHT WING TRAILING EDGE PANEL SUPPORT CORRODED AT STA 852. REMOVED AND REPLACED PANEL SUPPORT IAW ENGINERRING ORDER REA 47369FAB02 AND SRM 51-40-02 PARA 4 AND 7.

Part: RETAINER — CORRODED (LT WING) · corrosion level 2 · airframe 85,902 hrs · 39,542 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 57-572-00-01, LOWER WING TRAILING EDGE LOWER PANEL NEAR O/B FLAP O/B FAIRING HAS A CORRODED SEAL RETAINER. REPAIRED LOWER WING TRAILING EDGE LOWER PANEL SUPPORT BEAM IAW ENGINEERING ORDER 4736REA07 AND SRM 51-40-02.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 85,902 hrs · 39,542 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 71-828-00-01-O/B T/R UPPER SLIDE TRACK FAIRING IS BENT AND CHAFFED. REMOVED AND REPAIRED ON ENGINEERING ORDER 47369REA03.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 85,902 hrs · 39,542 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 55-434-00-01. BLENDED CORROSION OUT OF LIMITS. NOMINAL T=.140" REMAINING T=.080" REPAIRED BLENDED AREA IAW ENGINEERING DOC 4736REA04 REV IR AND SRM 51-10-01/FIG 201 REPAIR 6.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 85,902 hrs · 39,542 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VIST. FINDING: TASK CARD 57-572-00-02-RIGHT WING TRAILING EDGE BONDED PANEL LEADING EDGE IS BULGING WS 1050. REMOVED UPPER RIGHT WING TRAILING EDGE PANEL FOR FURTHER INSPECTION, FOUND CORROSION ON UPPER WING SKIN. CLEANED CORROSION AND REMOVED .032", REMAINING .059 FOUND TO BE OUT OF LIMITS IAW STRUCTURES REPAIR MANUAL 51-40-02 FIG 101/TABLE 1. REPAIRED RIGHT FIXED WING PANEL ASSEMBLY IAW ENGINEERING ORDER 4736REA01. REINSTALLED UPPER SKIN PANEL IAW SRM 51-40-02.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 81,635 hrs · 38,100 cycles

FLIGHT ATN3706 EN ROUTE FROM DEPARTURE STATION KABE TO DESTINATION STATION KONT EICAS MESSAGE DISPLAYED "R OIL FILTER". AS DIRECTED BY QRH, THE RIGHT ENGINE WAS SHUTDOWN. NOTIFIED ATC, DECLARED EMERGENCY. DIVERSION TO KILN. LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT GROUNDED FOR CORRECTIVE ACTION. EVIDENCE OF METAL FOUND IN C SUMP. REMOVED AND REPLACED RIGHT ENGINE. ENGINE RUNS SATISFACTORY. NO DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,456 hrs · 38,038 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT SIDE OF FRAME AT STATION 742 OUTBOARD STRINGER 39R IS CORRODED. REMOVED AND REPLACED SHEAR TIE AND CLIP FROM FORWARD LOWER CARGO STATION 742 STRINGER 39R WITH NEW PART IN ACCORDANCE WITH DRAWING 143T1214.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,456 hrs · 38,038 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER KEEL WEB IN THE RIGHT MAIN LANDING GEAR WHEEL WELL HAS AREAS OF CORROSION IN THE FORWARD PASS THROUGH LOCATION. BLENDED CORROSION ON RIGHT MAIN LANDING GEAR WHEEL WELL STATION 970 RIGHT BUTT LINE 5 FOUND TO BE OUT OF LIMITS. NORMAL: .050, REMAINING: .020. FABRICATED DOUBLER REPAIR USING 7075 T6 .080 IN ACCORDANCE WITH SRM 51-10-02 PARAGRAPH 15, ENGINEERING DOCUMENT 4726REAO1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,456 hrs · 38,038 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STATION 859.5 LEFT BUTT LINE 89 BELOW WATER LINE 200, FRAME INNER CHORD TRANSITION RADIUS CRACKED .25" APPROXIMATELY. REMOVED FASTENERS PER JOB CARD ENGINEERING ORDER 53-767-5352 FOR HIGH FREQUENCY EDDY CURRENT. COMPLIED WITH STATION 859.5 LEFT BUTT LINE 89 WATER LINE 200 FRAME INNER CHORD RADIUS CRACK IN ACCORDANCE WITH JOB CARD ENGINEERING ORDER 53-767-5352.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 79,529 hrs · 37,351 cycles

DURING MX VISIT ACCOMPLISHED PERMANENT REPAIR FOR THE SHEAR TIE ATTACHED TO THE LT LONGERON LOCATED AT STATION 1746.25 & WL 258.44. WORK WAS ACCOMPLISHED IAW ENGINEERING DOCUMENT 53-767-5445 DATED 04 08 16 REV 3, NR0001, APPROVED REPAIR ON 8110-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,788 hrs · 37,076 cycles

SKIN CRACK & PROBABLE CORROSION AT APPROX FS 1339, LONGERON 35L. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED REPAIRED PARTS IAW SRM 51-30-01. COMPLIED WITH HFEC OF AREA WHERE DAMAGE WAS REMOVED IAW NDT PART 6 51-00-19. NO DEFECTS NOTED.

Part: CAP — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HVY MX. UPPER CAP ON LE RIB AT LES 261 CORRODED 4 INCHES FROM FRONT SPAR ON INBD SIDE. REMOVED, REPAIRED & INSTALLED UPPER RIB CAP LES 261 IAW SRM 57-41-09 & 51-40-02.

Part: SPAR CAP — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. WING LE FRONT SPAR UPPER CAP CORRODED AT WING LES 579. R & R SPAR CAP IAW REA 47089REA19.

Part: SPAR CAP — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

WING LE FRONT SPAR UPPER CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP FROM LES 450 - 506 IAW EO 47089REA18.

Part: SKIN PANEL — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER WING SURFACE AT STATION 187 REAR SPAR AREA PANEL IS BULGED UP. POSSIBLE SIGNS OF CORROSION UNDER PANEL. REMOVED CORROSION IAW SRM 57-20-1 FIG 101. REMOVED & INSTALLED FASTENERS IAW AM 28-11-00. LEAK CHECKED SATISFACTORY.

Part: HINGE FITTING — CRACKED (RT MLG) · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FWD FITTING AT BODY DOOR CTR HINGE BEAM CRACKED. R & R RT MLG DOOR HINGE FITTING AT CTR BEAM TO DOOR CTR IAW SRM 51-40-02. OPERATIONAL CHECKED SATISFACTORY. NO LEAKS NOTED IAW AMM 32-32-12.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. AFT LOWER CARGO COMPARTMENT DOOR CUT OUT FOR PANEL 822D HAS A DAMAGED COUNTER SINK. REPAIRED DAMAGED SCREW HOLE IAW ENGINEERING DOCUMENT 47129REA04. REINSTALLED PANEL 822D IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON LOWER PORTION OF BODY FITTING AT STATION 933 RT SIDE IN UPPER CARGO. INSTALLED NEW STUB FITTING AT RT STATION 933 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 478) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FLOORBEAM UPPER TEE CORRODED AT BS 478, RBL 5 TO 9 AROUND NUTPLATES ON LOWER SURFACE. R & R FLOORBEAM UPPER TEE IAW DWG 143T 1202 & SRM 53-30-07 SEC 43.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. FLOOR FRAME UPPER CHORD HAS CORROSION UNDER NUTPLATES AT STATION 676, RBL 17 TO 19 LOWER SURFACE. FABRICATED, R & R FLOOR FRAME UPPER CHORD IAW DWG 143T 1211 & SRM 53-30-07 SEC 43 FIG 1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON STRINGER 36R AT STATION 445. R & R STRINGER 36R STATION 434 - 466 IAW REA 47089REA08.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. UPPER CARGO STATION 676 AFT OF SPLICE ON STRINGER 11L IS CRACKED. REMOVED, FABRICATED & INSTALLED NEW STRINGER IAW ENGINEERING DOCUMENT 4712REA03 & SRM 53-00-03.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1043 CTR FLOORBEAM ATTACH FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1021 CTR FLOORBEAM FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FUSELAGE SKIN GOUGED IN TWO PLACES AT AFT END OF UPPER HORSE COLLAR FS 1804 - 1815. REPAIRED DAMAGED FWD SKIN IAW ENGINEERING DOCUMENT REA 47129REA02. REPAIRED DAMAGED AFT SKIN IAW SRM 53-80-01 & ENGINEERING DOCUMENT REA47129REA02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 OUTER CHORD LOWER TENSION FITTING, TENSION BOLT HOLE ELONGATED. REPLACED RT LOWER FWD STATION 1809.5 TENSION FITTING IAW SRM 51-40-02 & EO 53-767-4857.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SKIN HAS HFEC OPEN HOLE DEFECT INDICATION AT FWD LOWER HOLE, COMMON TO CHORD, SPLICE FITTING & TENSION FITTING. INTERIOR SURFACE AROUND HOLE HAS CORROSION. DAMAGED AREA WAS REPAIRED IAW SRM 53-80-01 REPAIR 3 & ENGINEERING DOCUMENT 47129REA02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SPLICE FITTING LOWER TENSION BOLT HOLE HAS HFEC OPEN HOLE DEFECT INDICATION. R & R SPLICE FITTING IAW SRM 51-40-02 & EO 53-767-4857.

Part: SPLICE PLATE — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. WING LE FRONT SPAR UPPER SPAR CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP, UPPER SPLICE PLATE, FROM LES 450 - 506 IAW 47089REA18.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD UPPER TENSION FITTING HAS DAMAGED HOLE, COMMON TO SPLICE FITTING & SKIN. RT UPPER FWD STATION 1809.5 TENSION FITTING WAS REPLACED IAW SRM 51-40-02 & EO 53-767-4857. FITTING FABRICATED IAW ENGINEERING DOCUMENT 47089FAB14.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. STRUCTURE BEHIND LT PICKLE FORK SHOWS SIGNS OF CORROSION. R & R CORRODED BEARING PLATE IAW SRM 51-40-02 & EO 47008ORD11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 368, RBL 23 UNDERSIDE OF UPPER CHORD IS CORRODED AT NUTPLATE LOCATION. R & R UPPER CHORD IAW BDWG 143T1202 & SRM 51-40-02. PRIMED & TOP COAT FINISH APPLIED IAW AMM 51-21-10-7.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 544, RLB 34 UNDER BILGE COVER FOR LATERAL GUIDE, 1R ATTACH ANGLE CORRODED AS SEEN WITH MIRROR. R & R ANGLE IAW SRM 51-40-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. CORROSION AT NUTPLATES ON KEEL PANEL ATTACH TEE STATION 961. R & R TEE, KEEL BEAM FAIRING SPLICE IAW DWG 145T8629.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. CORROSION AT STATION 1043 TO 1059, LBL 98, 18 INCHES FROM UPPER PRESS PANEL. LONGERON REPLACED. REMOVED & INSTALLED MOST INBD AFT BONDED PANEL IAW SRM 51-40-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. CORROSION UNDER NUTPLATES ON KEEL PANEL ATTACH CROSS MEMBER AT STATION 918. R & R KEEL BEAM TEE SPLICE STATION 918 IAW SRM 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FLOOR FRAME UPPER CHORD CORRODED AT STATION 1263, LBL 31 AROUND NUTPLATES. R & R STATION 1263 FLOORBEAM UPPER CHORD IAW SRM 51-40-02 & DWG 146T1208.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 742, LBL 17 FLOOR SUPPORT ANGLE IS CORRODED TOP & BOTTOM. INSTALLED FLOOR SUPPORT ANGLE AT STATION 742 FROM LBL 43 TO RBL 43 IAW SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FLOOR FRAME UPPER CHORD CORRODED STATION 1175, RBL 24 LOWER SURFACE. INSTALLED WEB IAW SRM 51-40-02. FABRICATED & INSTALLED REPLACEMENT FRAME UPPER CHORD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 595, LBL 33 UNDERNEATH THE BILGE COVER FOR PDU 7L, AFT OTBD NUTPLATE HAS CORROSION AROUND IT. R & R INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 549, LBL 37 AFT OTBD NUTPLATE, ON UNDERSIDE FOR LATERAL GUIDE IS 1L IS CORRODED. R & R FLOOR SUPPORT 143T5000-86 IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. STRINGER 36L CORRODED AT STRINGER SPLICE STATION 1307. SPLICED IN REPLACEMENT SECTIONS OF STRINGERS IAW SRM 53-00-03 FIG 201 REPAIR 2 FROM STATION 1231 TO 1340.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. OTBD SIDE OF STRINGER 35L AT STATION 1307 HAS CORROSION ON AFT EDGE AT TRANSITION TO FITTING. SPLICED IN REPLACEMENT SECTION OF STRINGER 35L IAW SRM 53-00-03 FIG 201 REPAIR 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

ACFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. INTERCOSTAL BETWEEN STATION 1263 & 1285, 3RD FROM ALC DOOR HAS CORROSION UNDER SEVERAL NUTPLATES. R & R CORRODED SUPPORT INTERCOSTAL IAW SRM 51-40-02 & DWG 146T5000.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. PANEL ATTACH CHANNEL BETWEEN STATION 1263 - 1285, LBL 28 CORRODED AROUND NUTPLATES ON LOWER SURFACE. INSTALLED PANEL ATTACH CHANNEL AT STATION 1263 - 1285, LBL 28 IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. STRINGER 25L CRACKED ON LOWER END AT SPLICE AT STATION 679. R & R STRINGER 25L FROM STATION 676 - 710 IAW SRM 53-00-03 FIG 2.

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. REAR SPAR WEB & REAR SPAR PAD UP AREAS CORROSION AT STATION 955 AT THE UPPER SECTION ABOVE BOLT HOLE 1 - C3 & BOTTOM SECTION AROUND BOLT HOLE 9 - 11. REMOVED CORROSION IAW SRM 57-10-10. AREA REQUIRED REPAIR & WAS REPAIRED IAW ENGINEERING DOCUMENT 47089REA27.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. LT SIDE FRAME FITTING CORROSION ON PRESS WEB ATTACH POINT & BELOW HOLE NR 9. INSTALLED SIDE FRAME FITTING IAW SRM 51-40-02 & ENGINEERING DOCUMENT 47008ORD11.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. CORROSION ON LT WING UPPER TE SPAR CAP STATION 825. REMOVED CORROSION & REPAIRED LT WING UPPER SKIN PANEL IAW ENGINEERING DOCUMENT 47089REA20.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. STRINGER 33L AT STATION 445 CORRODED IN POCKET. R & R STRINGER 33L FROM STATION 434 TO 466 IAW SRM 53-00-03 FIG 2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FOUND CORROSION AT STATION 456 ON SKIN UNDER STRINGER 38R. REMOVED DAMAGED AREA, 1 X 2. FABRICATED FROM 7075-T6. INSTALLED FILLER & REPAIR DOUBLER IAW SRM 51-40-02 & 53-30-01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. CORROSION IN STRINGER 38R POCKET STATION 420 TO 428. R & R STRINGER 38R FROM STATION 400 - 434 IAW SRM 51-40-02-4B & REA 47089REA15.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON STRINGER 38R FROM STATION 440 - 448. R & R STRINGER 38R FROM STATION 434 - 464 IAW SRM 51-40-02 PARA 2B.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. SIDE FRAME FITTING RT SIDE FOUND CORROSION AT PRESS DECK WEB HOLES & POCKETS. INSTALLED NEW SIDE FRAME FITTING IAW SRM 51-40-02 & ENGINEERING DOCUMENT 47008RD12.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER STRAP ON FRAME AT STATION 1269 IN ALC, FWD OF DOOR CUT OUT BETWEEN STRINGER 34R - 33R CORRODED. R & R FRAME STATION 1269 UPPER CAP IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT FOR HEAVY MX, FAILSAFE INSPECTION. CORROSION BETWEEN THE ALC DOOR JAMB SILL & THE UPPER PLATE BETWEEN STATION 1241 - 1263. R & R DOOR JAMB UPPER & LOWER SILL PLATES IAW SRM 51-40-02 & DWG 146T8048.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. SHEAR TIE CORRODED AT STATION 1270, STRINGER 36R. R & R SHEAR TIES IAW SRM 51-40-02. HEAT TREATED TO T6 TEP IAW 5602.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. UPPER SPAR CORRODED LT WING AT STATION 900 - 930. UPPER SPAR AT LT WING AT STATION 900 - 930 BLENDED IAW SRM 57-20-01 FIG 1 & 2. EACH DOUBLERS SHOT PEENED IAW REA 47089REA12.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND ON HEAVY MX, FAILSAFE INSPECTION. DOOR FRAME, ANGLE & BEAR STRAP CORRODED AT STATION 1270 BETWEEN STRINGER 34 & 35R. DOOR FRAME ANGLES & BEAR STRAP WERE REPAIRED IAW REA 87049REA13.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. LT FITTING BETWEEN STATION 933 - 955 BELOW STRINGER 21L HAS 1 HOLE ENLARGED FROM PREVIOUS REWORK & 2 HOLES TAKEN TO THE NEXT NOMINAL FOR CORROSION CLEAN UP. REPAIRED STIFFENER IAW ENGINEERING DOCUMENT 4708923. TREATED & PRIMED IAW 51-20-01.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. BULK CARGO AREA FLOOR SUPPORT CHANNEL AT STATION 1438 - 1461 AT 25" LBL HAS 2 CRACKED SPOTS. R & R BULK CARGO AREA FLOOR SUPPORT CHANNEL AT STATION 1438.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FOUND CORROSION ON FUSELAGE SKIN UNDER FAILSAFE STRAP BOTTOM RT SIDE AT STATION 995. REMOVED CORROSION FOUND OUT OF LIMITS COMPLIED WITH ENGINEERING DOCUMENT REA 4789REA24 & ORD 47008ORD10.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER CARGO AT STATION 1120 UNDER PANEL 251C, FWD SIDE A CORRODED BEAM. REMOVED, FABRICATED & REPLACED INTERCOSTAL IAW SRM 51-40-02 & 47089FAB11.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. CORROSION AT WS 800 UPPER SURFACE. REPAIRED LT WING UPPER SKIN PANEL & WS 800 IAW ENGINEERING DOCUMENT 47089REA22.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. WING TO TE UPPER PANEL SUPPORT BEAM AT STATION 285 CORRODED AROUND NUTPLATES. R & R CORRODED SUPPORT BEAM ON LT WING IAW 10136-3001-7075T6511 & DWG 113T1623.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. PERFORMED DETAILED INTERNAL INSPECTION OF UPPER CARGO LT SIDE SKIN AT STATION 955. CORROSION AT LOWER SIDE, SIDE FRAME FITTING. CLEANED AREA OF CORROSION & REPAIRED AREA IAW ENGINEERING DOCUMENT 470080RD & 47089REA21.

Part: RIB — CORRODED (RT WING) · airframe 78,323 hrs · 36,859 cycles

RIGHT WING FIXED LE STRUCTURE STATION 933 HAS LIGHT CORROSION ON INBD & OTBD AREAS. BLENDED CORROSION ON THE BOTTOM OF THE LE RIB AT STATION 933. CORROSION OUT OF LIMITS IAW SRM 57-41-09. REPLACED RIB IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HVY MX. REAR SPAR TO WING TE UPPER PANEL ATTACH BEAM UPPER CAP CORRODED AROUND NUTPLATES AT STATION 288. FABRICATED & INSTALLED UPPER CHORD IAW DWG 113T1623 & SRM 51-40-02.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR SCHEDULED HVY MX. WING LE UPPER RIB INBD OF TAI TELESCOPING DUCT CORRODED AT FWD & AFT UPPER SURFACES LOCATED LES 456. R & R RT WING LE UPPER RIB LOCATED AT LES 456 IAW DWG 114T2202.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

BULK CARGO DOOR SILL AREA UNDER SCUFF PLATE CORRODED AREA AT FLOOR. R & R BULK CARGO DOOR LOWER SILL FLOOR PLATE IAW SRM 51-40-02.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR SCHEDULED HVY MX. AFT FUSELAGE LOWER EXT SKIN HAS A LARGE CREASE 33 INCHES LONG AT BS 1439 FROM STRINGER 35L - 35. DAMAGE REPAIRED IAW SRM 53-00-01.

Part: STRINGER — CORRODED (BS 445) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

STRINGER 37L CORRODED IN POCKET AT BS 445. R & R STRINGER SECTION FROM BS 434 - 464 IAW SRM 53-00-03 & SRM 51-40-02 PARA 4B & 7A.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

CORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R OUT OF LIMITS. REPAIRED CORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R IAW 47089REA02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. ALC DOOR FRAME STRAP AT FS 1269 BETWEEN STRINGER 32 - 31 CORRODED AROUND FASTENER. INSTALLED NEW STRAP IAW SRM 51-40-02. SPLICE FABRICATED IAW REA 47089REA16.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. STRINGER 39L AT STATION 1373 CORRODED. REPAIRED STRINGER AT STATION 1373 STRINGER 39L IAW AMM 53-00-03.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

LEFT WING AT STATION APPROX 433 JUST FWD OF INBD AILERON BRACKET STRUCTURE WORN. R & R FITTING & BRACKET LT WING AT STATION 433 IAW SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. TOP FRAME CORD CORROSION AT STATION 1088. INSTALLED NEW FRAME CHORD BETWEEN STRINGER 34L - 34R IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. STRINGER 31R AT STATION 450 CORRODED IN POCKET. R & R STRINGER 31R FROM STATION 434 TO 466 IAW SRM 53-00-03 ENGINEERING DOCUMENT 47089REA14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER CARGO SECTION 46 AT STATION 1605 12" RBL C TRACK CORRODED. R & R SEAT TRACK IAW 47089FAB05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER CARGO SECTION 46 STATION 1605 AT 34 RBL C TRACK CORRODED. R & R SEAT TRACK IAW 47089FAB06.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR SCHEDULED MX, NO OPERATIONS. CORROSION ON BILGE PANEL AT STATION 544 LBL 20. REMOVED & FABRICATED NEW WEB STATION 522 - 544 LBL 10 - 30 IAW DWG 143T5000. INSTALLED WEB IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

STRINGER 39R CORRODED AT BS 1540 IN ALC. REPAIRED CORRODED STRINGER IAW SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

STRINGER 37L CORRODED AT STRINGER SPLICE STATION 1307. REMOVED & INSTALLED SERVICEABLE NEW SECTION AT STRINGER & SPLICE IAW SRM 53-00-03 FIG 201 REPAIR 2.

Part: ATTACH BRACKET — CRACKED (WING) · airframe 78,323 hrs · 36,859 cycles

REAR SPAR TO WING TE ATTACH BRACKET SPLITTING ON SIDE UNDER NUTPLATES AT WING STATION 1046. REPLACED CHORD OFF WING STATION 1046 IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

ACFT GNDED FOR SCHEDULED MX, NO OPERATIONS. STRINGER 32R AT STATION 452 CORRODED IN POCKET. REMOVED CORRODED SECTION OF STRINGER 32R FROM STATION 436 TO 466 & REPLACED WITH SERVICEABLE COMPONENT IAW REA 47089REA08-1 FIG 201.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

CORROSION ON ANGLE ON TOP SURFACE OF KEEL PANEL TO VERTICAL BEAM AT STATION 999. R & R VERTICAL BEAM AT STATION 999 IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. LT OTBD CHORD AREA 1 HAS CRACK INDICATIONS WITH ROTARY SCANNER & RING PROBE IN FWD LOWER HOLE & BOTH UPPER & LOWER AFT HOLES. R & R SPLICE FITTING IAW SRM 51-40-02. 1809.5 CHORD LOWER REPLACED IAW EO 53-767-4858.

Part: SUPPORT CHANNEL — CRACKED (NR 1 PYLON) · airframe 78,323 hrs · 36,859 cycles

THE INBD SUPPORT CHANNEL IS GOUGED. LOCATED INTERIOR OF 437BR NEAR STATION 280. R & R CHANNEL ON NR 1 PYLON IAW SRM 51-40-02.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 78,323 hrs · 36,859 cycles

NUMBER 2 FWD PYLON AT BLEED AIR DUCT INBD STRUCTURE AT ATTACHMENT IS CRACKED IN SEVERAL AREAS. WEB FABRICATED IAW DWG 311T1510. INSTALLED WEB IAW DWG 311T1510 & SRM 51-40-02.

Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 78,323 hrs · 36,859 cycles

NUMBER 2 FWD PYLON AT BLEED AIR DUCT INBD STRUCTURE AT ATTACHMENT IS CRACKED IN SEVERAL AREAS. FABRICATED & INSTALLED LOWER CHORD IAW DWG 311T1510 & IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. CORROSION ON SKIN UNDER STRINGER 33L STATION 445. SKIN REPAIRED IAW SRM 53-00-01.

Part: ATTACH FITTING — CORRODED (WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR HEAVY MX. WING TE LOWER PANEL ATTACH T CAP UNDER NR 7 SPOILER CORRODED. LOWER CHORD CORRODED BEYOND LIMITS. REPLACED LOWER CHORD IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 78,323 hrs · 36,859 cycles

LOWER FWD ATTACH ANGLE ON WEB AT THE BOTTOM OF THE VERTICAL COMMON TO PANEL 324AL HAS A .50 CRACK. R & R ANGLE IAW DWG 173T1302. INSTALLED ANGLE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT GNDED FOR SCHEDULED MX, NO OPERATIONS. CORROSION ON FLOORBEAM UPPER CHORD AT STATION 544 LBL 20. R & R UPPER CHORD AT STATION 544 LBL 17 - 43 IAW SRM 53-00-07.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

FLOORBEAM FRAME UPPER CHORD AT STATION 500 RBL 43 CORRODED AROUND NUTPLATES ON LOWER SURFACE. R & R UPPER CHORD AT STATION 500 LBL 43 TO RBL 43 IAW SRM 53-00-07.

Part: SUPPORT RIB — CORRODED (RT WING) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT WING UPPER INBD AFT I BEAM CORRODED. INSTALLED NEW UPPER INBD AFT SUPPORT RIB IAW SRM 51-40-02.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTIONS. CORROSION HORIZONTAL STAB CTR BOX UPPER SURFACE FRONT SPAR RBL 18 - 24. REMOVED CORROSION DAMAGE & FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW 47089REA01.

Part: STRINGER — CORRODED (ZONE 300) · corrosion level 2 · airframe 78,323 hrs · 36,859 cycles

CORROSION ON STRINGER 7 BETWEEN RIB 1L & 1R OUT OF LIMITS. REPAIRED IAW REQUEST FOR ENGINEERING ASSISTANCE DOCUMENT 47089REA02.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 78,323 hrs · 36,859 cycles

POSSIBLE CRACK COMING FROM NUTPLATE HOLE ON FWD LOWER FRAME OF BULK CARGO DOOR. REPAIRED AREA IAW SRM 51-70-13.

Part: INERTIA REEL — OUT OF POSITION · airframe 77,667 hrs · 36,598 cycles

EMERGENCY DESCENT DEVICE NR 1 FOUND EXTENDED. NR 1 EMERGENCY DESCENT DEVICE WAS REMOVED FROM THE ACFT. OPEN

Part: RELAY — INOPERATIVE · airframe 77,503 hrs · 36,532 cycles

TOTAL AIR TEMPERATURE PROBE HEAT INOPERATIVE DURING INITIAL CLIMB. ACFT RETURNED TO STATION. MX ISOLATED THE PROBLEM TO THE LT ENGINE 50 PERCENT RELAY K644. R & R RELAY K644 IAW WD 30-33-11. SYS CHECKED GOOD IAW AMM 30-33-00 AND DURING ENGINE RUN IAW ERH 02.01.18.

Part: SPINNER — DAMAGED (ENGINE) · airframe 76,758 hrs · 36,246 cycles

DURING TAKEOFF ROLL, THE ACFT HAD A VIBRATION ON THE RT ENGINE (BIRD STRIKE) AND THE CREW REJECTED TAKE OFF AT 100 KTS. THE ACFT RETURNED BACK TO THE GATE WHERE MX PERSONNEL PERFORMED A HIGH ENERGY STOP INSPECTION IAW AMM 5-51-14. FURTHER INSP OF THE RT ENGINE REVEALED DAMAGE TO FAN BLADES 11, 12, 13, 14 AND THE STATOR SEAL WAS LOOSE AT THE 2 O'CLOCK POSITION. THERE WAS NO DAMAGE TO THE TURBINE BLADES AND NO DEBRIS FOUND AT THE EXHAUST OR INLET SECTIONS. R & R SPINNER IAW AMM 72-31-01. R & R DAMAGED BLADES IAW AMM 72-31-02 AND PERFORMED TRIM BALANCE IAW AMM 72-31-00. OPS CHECKED GOOD. FAN VIBRATION AT 1.1 AT 97.6 N1.

Part: CIRCUIT BREAKER — FAILED · airframe 76,617 hrs · 36,181 cycles

AFTER TAKEOFF AIRCREW RECEIVED 2 EICAS MESSAGES. RT FORWARD FUEL PUMP FAULT AND LT AFT FUEL PUMP FAULT. RETURNED TO STATION. R & R RT FWD/ LT AFT CIRCUIT BREAKER M16 IAW WDM 28-22-11. OPS CHECKED GOOD.

Part: SENSOR — FAILED (RIGHT ENGINE) · airframe 76,485 hrs · 36,128 cycles

RIGHT ENGINE OIL TEMP HIGH, 185-200 DEGREES, OIL PRESSURE NORMAL AT 60. ENGINE WAS SHUTDOWN. PERFORMED FIM PROCEDURE 79-34 FAULT TREE 804 BLOCK 1. R & R OIL TEMP BULB IAW MM 79-34-01. CLEANED & RESECURED BACKSHELL. OPS AND LEAK CHECKED GOOD ON ENGINE RUN. NO DEFECTS NOTED.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 75,653 hrs · 35,766 cycles

DURING C19 CHECK INSPECTION, LT FUSELAGE - SECTION 48 - BODY STATION 1809.5 BULKHEAD FWD OUTER CHORD CRACK DAMAGE AT STA 1809.5. PERFORMED MAJOR REPAIR IAW SB 767-53A0078. REMOVED ALL ACCESS DOORS AND ALL FASTENERS FROM THE REPAIRED AREA IAW SB 767-53A0078, REV 6, FIG 3, METHOD 2 AND SRM 51-40-02. FABRICATED (04EA) FILLERS AND (04EA) PLATES OF AL 7075-T6 IAW SB 767-53A0078, PAGE 58, SHEET 6. CLEANED, TREATED AND PRIMED AREA, FILLERS AND PLATES IAW SRM 51-20-01. INSTALLED REPAIRED PARTS IAW SB 767-53A0078 IAW SRM 51-40-02 AND SRM 51-20-05 AND EO 2012039.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 75,653 hrs · 35,766 cycles

DURING C19 CHECK INSPECTION RT FUSELAGE - SECTION 48 - BODY STATION 1809.5 BULKHEAD FWD OUTER CHORD CRACK DAMAGE AT STA 1809.5. PERFORMED MAJOR REPAIR IAW SB 767-53A0078. REMOVED ALL ACCESS DOORS AND ALL FASTENERS FROM REPAIRED AREA IAW SB 767-53A0078 METHOD 2 AND SRM 51-40-02. FABRICATED FILLERS AND PLATES IAW S/B 767-53A0078 PAGE 58 SHEET 6. PERFORMED CRACK END STOP DRILL IAW SRM 51-10-00. CLEANED, TREATED AND PRIMED AREA, FILLERS AND PLATES IAW SRM 51-20-01. INSTALLED REPAIRED PARTS IAW SB 767-53A0078 IAW SRM 51-40-02 AND SRM 51-20-05 AND EO 2012040.

Part: FLOORBOARD — DAMAGED (BS 1065) · airframe 75,449 hrs · 35,679 cycles

DURING INSPECTION, FOUND FLOORBOARD DAMAGED AT STA NR 1065 LT. REPAIRED DAMAGED FLOORBOARD BEAM IAW EO 53-767-4838 R1.

Part: ESCAPE REEL — DISLODGED · airframe 75,137 hrs · 35,543 cycles

ON LANDING, THE FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES, FOUR INERTIAL ESCAPE REELS FEEL OUT. MAINTENANCE REPLACED ALL FOUR ESCAPE REEL DEVICES IAW AIRCRAFT MAINTENANCE MANUAL IAI SUPPLEMENT 25-61-03/401. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — PUNCTURED (ZONE 100) · airframe 75,087 hrs · 35,517 cycles

DURING GROUND HANDLING, HOLE IN PUNCTURED FUSELAGE FORWARD OF AFT CARGO DOOR AND A DENT AFT OF AFT CARGO DOOR. REPAIR INSTALLED IAW EO C00-6-53-391-11. ACFT RETURNED TO SERVICE.

Part: FAN — LACK OF LUBE (ZONE 400)

DURING TAKEOFF ROLL, THE LT ENGINE FAN VIBRATION 2.5. WHEN INFLIGHT AT 370 ENGINE VIBRATION IS 5.1. THE CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAN LUBE IAW AMM 72-31-02. AFTER FAN LUBE ENGINE VIBRATION AT .9, WITH IN LIMITS IAW ERH 01.01.0 APPENDEX C. ACFT WAS RETURNED TO SERVICE.

Part: DOOR — DISCONNECTED (NLG) · airframe 74,776 hrs · 35,383 cycles

DURING CLIMBOUT, THE RT NOSE GEAR DOOR WOULD NOT CLOSE. RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED NOSE GEAR AND FOUND THE RT AFT NLG DOOR DISCONNECTED. MX JACKED THE NOSE GEAR IAW AMM 07-11-02 TO RECONNECT DOOR AND ADJUST IAW AMM 32-22-04. OPS CHECKED GOOD IAW 32-22-04. ACFT WAS RETURNED TO SERVICE.

Part: SENSOR — OUT OF ADJUST (ZONE 800) · airframe 73,804 hrs · 34,958 cycles

DURING CRUISE FROM KMIA, THE CREW NOTICED EICAS MESSAGE CODE 52-71-06-16 FOR THE E/E DOOR. THEY ACCOMPLISHED CHECK LIST AND RETURNED TO KMIA WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE SENSOR FOR THE ELECTRONICS ACCESS DOOR. OPERATIONAL CHECK GOOD IAW BOEING AMM 52-71-00. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (STAB TRIM) · airframe 73,515 hrs · 34,829 cycles

DURING CRUISE, NOTICE EICAS MESSAGE WITH CODE 27-48-03-00 STABILIZER TRIM DISPLAYED AND STABILIZER TRIM LIGHT ILLUMINATED WITH STABILIZER TRIM OPERATES AT HALF SPEED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED PROCEDURES IN FIM 27-48-00, FIG 106, BLOCKS 1,2,3 AND 63, NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.